|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
radio and telemetry
|
|
gptkbp:controls
|
automated and manual
|
|
gptkbp:crew
|
Cosmonaut training
|
|
gptkbp:crewCapacity
|
3
yes
|
|
gptkbp:crewSize
|
yes
|
|
gptkbp:decommissioned
|
1971
|
|
gptkbp:design
|
manned missions
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:diedIn
|
yes
|
|
gptkbp:environmentalImpact
|
yes
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_1
gptkb:Soyuz_10
1967-11-28
1971-10-30
|
|
gptkbp:height
|
7.2 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 7K-T
|
|
gptkbp:launchDate
|
1967-11-28
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
6800 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_rocket
none
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:majorRivers
|
10
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mission
|
manned spaceflight
|
|
gptkbp:navigationEquipment
|
inertial and ground-based
|
|
gptkbp:notableFeature
|
Soyuz_1,_Soyuz_2,_Soyuz_3
|
|
gptkbp:numberOfFigures
|
10
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:orbitalInclination
|
yes
28,000 km/h
|
|
gptkbp:payloadCapacity
|
up to 300 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:primaryFunction
|
transport to space station
|
|
gptkbp:productionYears
|
1967-1971
|
|
gptkbp:propulsion
|
liquid fuel engines
|
|
gptkbp:replacedBy
|
gptkb:Soyuz_7K-OK
|
|
gptkbp:respondsTo
|
yes
|
|
gptkbp:secondaryMission
|
10
|
|
gptkbp:services
|
yes
|
|
gptkbp:significantEvent
|
first crewed flight of Soyuz series.
|
|
gptkbp:successor
|
gptkb:Soyuz_7K-OK
|
|
gptkbp:usedFor
|
gptkb:Soyuz_program
|
|
gptkbp:width
|
2.2 m
|